ES2276935T3 - Panel de aeronave. - Google Patents

Panel de aeronave. Download PDF

Info

Publication number: ES2276935T3
Authority: ES; Spain
Prior art keywords: panel; members; grid; metal cladding; core material
Prior art date: 2001-06-07
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Expired - Lifetime

Application number

ES02728286T

Other languages

English (en)

Spanish (es)

Inventor

Mats Folkesson

Stefan Thuresson

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Saab AB

Original Assignee

Saab AB

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

2001-06-07

Filing date

2002-04-30

Publication date

2007-07-01

2002-04-30 Application filed by Saab AB filed Critical Saab AB

2007-07-01 Application granted granted Critical

2007-07-01 Publication of ES2276935T3 publication Critical patent/ES2276935T3/es

2022-04-30 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

Links

239000000463 material Substances 0.000 claims abstract description 24
239000011162 core material Substances 0.000 claims abstract description 21
238000010276 construction Methods 0.000 claims abstract description 8
238000005253 cladding Methods 0.000 claims description 35
229910052751 metal Inorganic materials 0.000 claims description 35
239000002184 metal Substances 0.000 claims description 35
230000003014 reinforcing effect Effects 0.000 claims description 7
230000002787 reinforcement Effects 0.000 abstract description 10
229910052782 aluminium Inorganic materials 0.000 description 13
XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 13
238000004519 manufacturing process Methods 0.000 description 6
239000002131 composite material Substances 0.000 description 4
239000006260 foam Substances 0.000 description 4
238000000034 method Methods 0.000 description 4
238000009434 installation Methods 0.000 description 3
230000008901 benefit Effects 0.000 description 2
239000011248 coating agent Substances 0.000 description 2
238000000576 coating method Methods 0.000 description 2
230000000694 effects Effects 0.000 description 2
230000006870 function Effects 0.000 description 2
230000002829 reductive effect Effects 0.000 description 2
230000003068 static effect Effects 0.000 description 2
229920000049 Carbon (fiber) Polymers 0.000 description 1
230000006978 adaptation Effects 0.000 description 1
239000004917 carbon fiber Substances 0.000 description 1
150000001875 compounds Chemical class 0.000 description 1
230000008094 contradictory effect Effects 0.000 description 1
230000007797 corrosion Effects 0.000 description 1
238000005260 corrosion Methods 0.000 description 1
230000001419 dependent effect Effects 0.000 description 1
238000001514 detection method Methods 0.000 description 1
239000003822 epoxy resin Substances 0.000 description 1
239000003517 fume Substances 0.000 description 1
LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
238000009413 insulation Methods 0.000 description 1
239000012212 insulator Substances 0.000 description 1
238000002955 isolation Methods 0.000 description 1
VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
238000012986 modification Methods 0.000 description 1
230000004048 modification Effects 0.000 description 1
230000036961 partial effect Effects 0.000 description 1
239000002984 plastic foam Substances 0.000 description 1
229920000647 polyepoxide Polymers 0.000 description 1
230000008439 repair process Effects 0.000 description 1
230000007480 spreading Effects 0.000 description 1
238000003892 spreading Methods 0.000 description 1
230000001988 toxicity Effects 0.000 description 1
231100000419 toxicity Toxicity 0.000 description 1
230000003313 weakening effect Effects 0.000 description 1

Classifications

- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/046—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of foam
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2250/00—Layers arrangement
- B32B2250/03—3 layers
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/304—Insulating
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/56—Damping, energy absorption
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/24—Aluminium
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft

Landscapes

Engineering & Computer Science (AREA)
Mechanical Engineering (AREA)
Aviation & Aerospace Engineering (AREA)
Laminated Bodies (AREA)
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

ES02728286T 2001-06-07 2002-04-30 Panel de aeronave. Expired - Lifetime ES2276935T3 (es)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
SE0102083A SE519185C2 (sv)	2001-06-07	2001-06-07	Flygplanspanel
SE0102083		2001-06-07

Publications (1)

Publication Number	Publication Date
ES2276935T3 true ES2276935T3 (es)	2007-07-01

Family

ID=20284451

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
ES02728286T Expired - Lifetime ES2276935T3 (es)	2001-06-07	2002-04-30	Panel de aeronave.

Country Status (7)

Country	Link
US (1)	US7025305B2 (de)
EP (1)	EP1399362B1 (de)
AT (1)	ATE346789T1 (de)
DE (1)	DE60216454T2 (de)
ES (1)	ES2276935T3 (de)
SE (1)	SE519185C2 (de)
WO (1)	WO2002098734A1 (de)

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US7210655B2 (en) *	2004-12-03	2007-05-01	The Boeing Company	Reconfigurable interior sidewall
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GB2428417B (en) *	2005-10-27	2007-09-12	Hal Errikos Calamvokis	Aircraft fuselage structure
US7766277B2 (en) *	2006-01-19	2010-08-03	The Boeing Company	Deformable forward pressure bulkhead for an aircraft
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DE102007003277B4 (de) *	2007-01-23	2012-08-02	Airbus Operations Gmbh	Rumpf eines Luft- oder Raumfahrzeuges in CFK-Metall Hybridbauweise mit einem Metallrahmen
DE102007003275B4 (de) *	2007-01-23	2013-11-28	Airbus Operations Gmbh	Schalenelement als Teil eines Flugzeugrumpfes
DE102007019821B4 (de)	2007-04-26	2012-11-22	Airbus Operations Gmbh	Strukturelement eines Flugzeugrumpfs
US8388795B2 (en)	2007-05-17	2013-03-05	The Boeing Company	Nanotube-enhanced interlayers for composite structures
DE102007030026A1 (de) *	2007-06-29	2009-01-02	Airbus Deutschland Gmbh	Strukturbauteil mit Spant- und Querträgerelement
US8042767B2 (en) *	2007-09-04	2011-10-25	The Boeing Company	Composite fabric with rigid member structure
ES2342866B1 (es) *	2007-11-30	2011-05-18	Airbus España, S.L.	Fuselaje de aeronave resistente a impactos.
US8038099B2 (en) *	2008-04-30	2011-10-18	The Boeing Company	Bonded metal fuselage and method for making the same
US20100155533A1 (en) *	2008-12-23	2010-06-24	Spirit Aerosystems, Inc.	Composite forward pressure bulkhead
FR2943311B1 (fr) *	2009-03-19	2011-03-04	Airbus France	Raidisseurs sous bavette pour aeronef
DE102009015856B4 (de) *	2009-04-01	2012-01-26	Airbus Operations Gmbh	Rumpfsegment und Verfahren zur Herstellung des Rumpfsegments
ES2396328B1 (es) *	2010-06-30	2014-02-06	Airbus Operations, S.L.	Fuselaje de aeronave en material compuesto y procedimientos para su fabricación.
EP2404824B1 (de) *	2010-07-08	2015-09-09	Airbus Opérations SAS	Luftfahrzeugstruktur und Herstellungsverfahren für eine solche Struktur
GB201012552D0 (en) *	2010-07-23	2010-11-17	Bae Systems Plc	Aircraft thermal insulation
DE102010038408B4 (de) *	2010-07-26	2020-11-19	Airbus Operations Gmbh	Strukturelement für ein Luft- und Raumfahrzeug und Verfahren zum Herstellen eines derartigen Strukturelementes
JP5535957B2 (ja) *	2011-02-21	2014-07-02	三菱航空機株式会社	翼パネルの形成方法
US8851422B2 (en) *	2012-08-28	2014-10-07	The Boeing Company	Bonded composite aircraft wing
US8985512B1 (en)	2012-09-21	2015-03-24	The Boeing Company	Aircraft, fuselages, and associated methods
EP2842865B1 (de) *	2013-08-28	2019-12-18	Airbus Operations GmbH	Fensterscheibe für ein flugwerk und verfahren zur herstellung davon
GB2528080A (en) *	2014-07-08	2016-01-13	Airbus Operations Ltd	Structure
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EP3281861B1 (de) *	2016-08-11	2019-10-02	AIRBUS HELICOPTERS DEUTSCHLAND GmbH	Drehflügler mit einem rumpf mit mindestens einem strukturell versteiften paneel
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2001
- 2001-06-07 SE SE0102083A patent/SE519185C2/sv not_active IP Right Cessation
2002
- 2002-04-30 ES ES02728286T patent/ES2276935T3/es not_active Expired - Lifetime
- 2002-04-30 DE DE60216454T patent/DE60216454T2/de not_active Expired - Lifetime
- 2002-04-30 EP EP02728286A patent/EP1399362B1/de not_active Expired - Lifetime
- 2002-04-30 WO PCT/SE2002/000843 patent/WO2002098734A1/en not_active Ceased
- 2002-04-30 AT AT02728286T patent/ATE346789T1/de not_active IP Right Cessation
- 2002-04-30 US US10/479,800 patent/US7025305B2/en not_active Expired - Lifetime

Also Published As

Publication number	Publication date
US7025305B2 (en)	2006-04-11
DE60216454T2 (de)	2007-09-27
EP1399362A1 (de)	2004-03-24
US20040155148A1 (en)	2004-08-12
DE60216454D1 (de)	2007-01-11
ATE346789T1 (de)	2006-12-15
SE0102083L (sv)	2002-12-08
EP1399362B1 (de)	2006-11-29
WO2002098734A1 (en)	2002-12-12
SE0102083D0 (sv)	2001-06-07
SE519185C2 (sv)	2003-01-28

Publication	Publication Date	Title
ES2276935T3 (es)	2007-07-01	Panel de aeronave.
ES2214520T3 (es)	2004-09-16	Un estratificado compuesto.
ES2450054T3 (es)	2014-03-21	Panel elástico para aeronaves
RU2576647C2 (ru)	2016-03-10	Конструктивный узел воздушного судна
US8177166B2 (en)	2012-05-15	Tail structure for an aircraft or spacecraft
CN101511674B (zh)	2012-06-13	用于飞行器的舱门框
US8123167B2 (en)	2012-02-28	Impact resistant aircraft leading edge structures and aircraft including the same
ES2822933T3 (es)	2021-05-05	Estructura de panel para una aeronave y procedimiento de fabricación de la misma
CN104507806B (zh)	2016-12-28	飞行器立体空间集成型附接装置
US10286956B2 (en)	2019-05-14	Motor vehicle
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US9359085B2 (en)	2016-06-07	Aircraft with fuselage-mounted engines and an internal shield
ES2310249T3 (es)	2009-01-01	Proteccion contra el impacto de un rayo y toma de tierra de un panel de aeronave compuesto.
US8844869B2 (en)	2014-09-30	Aircraft structural assembly and associated assembling method
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US11794873B2 (en)	2023-10-24	Auxiliary power unit enclosure and method of making the same
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US20080283664A1 (en)	2008-11-20	Aircraft Fuselage Structure
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US20180002107A1 (en)	2018-01-04	Lightweight flame resistant composite panel and panel attachment system
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